Patents Assigned to Lockheed Missiles & Space Company, Inc.
  • Patent number: 4702569
    Abstract: A method is described for selecting optical materials to use in designing color-corrected optical systems. Various dioptric, catadioptric and anamorphic optical systems are described, which use only two different types of optical materials to obtain precise axial color correction at three, four or five wavelengths (depending upon the particular optical materials), with only very small chromatic aberration occurring at wavelengths between the precisely color-corrected wavelengths. Examples of color-corrected lens systems comprising more than two glasses are also described.
    Type: Grant
    Filed: June 16, 1986
    Date of Patent: October 27, 1987
    Assignee: Lockheed Missiles & Space Company, Inc.
    Inventor: Romeo I. Mercado
  • Patent number: 4692388
    Abstract: Hydrogenated boron-silica alloy films having unexpected properties permitting in one embodiment the bonding together of metal and ceramic substrates by coating the surfaces to be bonded with the film mating the surfaces and heat treating the mated surfaces to expell hydrogen therefrom and to react to resulting boron-silicon alloy film with the substrates to form a liquid reaction product which forms a surface bond with the substrates or is at least partially absorbed in the substrates. In another embodiment, at least one surface of an intermetallic compound formed from elements selected from groups III and V of the periodic table is sealed against structural degradation by forming on the surface a solid boron-silicon-hydrogen alloy film. In still another embodiment, metal and organic resin substrates are protected against attack by water vapor, dissociated oxygen and molecular oxygen by forming a solid boron-silicon-hydrogen alloy film on the substrates.
    Type: Grant
    Filed: December 2, 1986
    Date of Patent: September 8, 1987
    Assignee: Lockheed Missiles & Space Company, Inc.
    Inventors: Henry W. Lavendel, John C. Robinson
  • Patent number: 4689104
    Abstract: Hydrogenated boron-silicon alloy films having unexpected properties permitting in one embodiment the bonding together of metal and ceramic substrates by coating the surfaces to be bonded with the film mating the surfaces and heat treating the mated surfaces to expell hydrogen therefrom and to react to resulting boron-silicon alloy film with the substrates to form a liquid reaction product which forms a surface bond with the substrates or is at least partially absorbed in the substrates. In another embodiment, at least one surface of an intermetallic compound formed from elements selected from groups III and V of the periodic table is sealed against structural degradation by forming on the surface a solid boron-silicon-hydrogen alloy film. In still another embodiment, metal and organic resin substrates are protected against attack by water vapor, dissociated oxygen and molecular oxygen by forming a solid boron-silicon-hydrogen alloy film on the substrates.
    Type: Grant
    Filed: June 24, 1985
    Date of Patent: August 25, 1987
    Assignee: Lockheed Missiles & Space Company, Inc.
    Inventors: Henry W. Lavendel, John C. Robinson
  • Patent number: 4687332
    Abstract: A scan-shear interferometer comprises a beamsplitter (11) for dividing an optical beam into a transmitted component I and a reflected component II, which are propagated in opposite directions along a triangular portion of an optical path defined by mirrors (12) and (13) back to the beamsplitter (11), from which the beam component I is transmitted and the beam component II is reflected to a mirror (14), which reflects the beam components I and II coincidentally to form pupils on an interference plane at a photodetector device (15). A rotating prism (16) is positioned so that each of the beam components I and II makes a double pass through the prism (16) before reaching the interference plane. Rotation of the prism (16) causes the pupil formed by the beam component II to remain stationary, and causes the pupil formed by the beam component I to move across the stationary pupil along a scan axis on the interference plane.
    Type: Grant
    Filed: October 15, 1985
    Date of Patent: August 18, 1987
    Assignee: Lockheed Missiles & Space Company, Inc.
    Inventor: Noah Bareket
  • Patent number: 4681407
    Abstract: A photographic objective comprising six lens elements is well-corrected for both monochromatic and chromatic aberrations, and is color-corrected at four wavelengths in a band extending from the visible to the near infrared regions of the electromagnetic spectrum with only negligible secondary and high-order spectra at wavelength between those for which color correction is achieved. The design form for the objective has been optimized for a focal length of 200 mm at an aperture ratio of f/4 and a field of view of 12.degree. without vignetting.
    Type: Grant
    Filed: December 2, 1985
    Date of Patent: July 21, 1987
    Assignee: Lockheed Missiles & Space Company, Inc.
    Inventor: Romeo I. Mercado
  • Patent number: 4679961
    Abstract: A mechanism for coupling a strut (30) to a nodal element (32) comprises a female coupling fixture (31) and a male coupling fixture (33). The female coupling fixture (31) includes an elongate cylindrical member (35), a distal end of which is hemicylindrically configured with an inner surface that is contoured to receive a conjugately contoured knob on a distal end of the male coupling fixture (33) in mating engagement. The female coupling fixture (31) also includes a sleeve (36), which is slidable coaxially from an OPEN position around an intermediate portion of the cylindrical member (35) to a LOCKED position around the matingly engaged distal ends of the cylindrical member (35) and the male coupling fixture (33). Spring-biases locking bars (50) and (51) maintain the sleeve (36) in the LOCKED position.
    Type: Grant
    Filed: June 16, 1986
    Date of Patent: July 14, 1987
    Assignee: Lockheed Missiles & Space Company, Inc.
    Inventor: James P. Stewart
  • Patent number: 4668867
    Abstract: A sample 10 of a composite material, such as a graphite-epoxy composite, is exposed to radiation in three distinct energy bands emanating from sources 12, 13 and 14, respectively. Corresponding detectors 16, 17 and 18 are positioned to measure the amount of energy in each band transmitted through the sample. Weight percentages of three different constituents of the sample 10 are calculated from a relatively simple algorithm whose variables include a ratio for each of said energy bands of the amount of energy that would be detected if the sample were not present in the radiation to the amount of energy transmitted through the sample when the sample is exposed to the radiation.
    Type: Grant
    Filed: May 28, 1985
    Date of Patent: May 26, 1987
    Assignee: Lockheed Missiles & Space Company, Inc.
    Inventor: Dean E. Lingenfelter
  • Patent number: 4653921
    Abstract: A real-time radial shear interferometer for monitoring the quality of the wavefront of an optical beam comprises (with reference to FIG. 3) a pair of beamsplitters (40, 45) and a pair of beam-folding mirrors (44, 46) arranged in Mach-Zehnder format. An afocal telescope (41) and a diffraction grating (30) cause a transmitted component of the beam to be separated into a plurality of diffraction maxima, and an afocal telescope (47) and a diffraction grating (31) cause a reflected component of the beam to be separated into a plurality of diffraction maxima. Diffraction beams formed from the transmitted component of the beam are combined with corresponding diffraction beams formed from the reflected component of the beam to produce a zeroth-order interferogram and positive and negative first-order interferograms.
    Type: Grant
    Filed: September 9, 1985
    Date of Patent: March 31, 1987
    Assignee: Lockheed Missiles & Space Company, Inc.
    Inventor: Osuk Y. Kwon
  • Patent number: 4654636
    Abstract: A shaft angle encoder comprises a code disc (21) mountable coaxially upon a rotary shaft (20) whose angular position is to be continuously measured. Coarse-bit angular position data are encoded digitally in Gray code by a pattern of opaque and transparent sectors provided on a plurality of inner annular tracks on the code disc (21). Fine-bit angular position data are encoded in analog triangular waveforms generated by the outermost annular track on the code disc (21). The analog position data are converted to fine-bit digital values, which are combined with coarse-bit digital values to obtain an angular position measurement. Alignment of the fine-bit digital values with the coarse-bit digital values obtained from the Gray code position data is accomplished by using information provided by overlapping the least significant bit of the coarse-bit digital values with the most significant bit of the fine-code digital values.
    Type: Grant
    Filed: January 9, 1986
    Date of Patent: March 31, 1987
    Assignee: Lockheed Missiles & Space Company, Inc.
    Inventor: Stanley J. Rusk
  • Patent number: 4639669
    Abstract: A procedure for nondestructively determining a physical characteristic of a test object (10) involves introducing an electromagnetic energy pulse into the test object, and measuring elapsed time before the signature of a time-dependent function of the energy thereby propagated through the test object (10) reaches a value larger than a pre-set threshold value. For example, the volume density of graphite fibers in a graphite-epoxy composite material can be determined by introducing a pulse of radio-frequency electromagnetic energy into the composite material, and by measuring the elapsed time before the voltage signature of the energy propagated through the composite material reaches a value larger than the threshold value.
    Type: Grant
    Filed: September 26, 1983
    Date of Patent: January 27, 1987
    Assignee: Lockheed Missiles & Space Company, Inc.
    Inventors: Darryl A. Howard, Lawrence Y. L. Shen
  • Patent number: 4637725
    Abstract: An interferometer in Mach-Zehnder configuration comprises beamsplitters (10, 12) and mirrors (11, 13), which divide an optical beam whose wavefront is to be monitored into an information component and a reference component, and which recombine the information and reference components to form an interference pattern that changes dynamically at a spatial light modulator (14) in response to dynamic variations in the atmosphere through which the beam passes. A spatial light filter (15) comprising a plate with a pin-hole aperture is positioned to transmit the reference component of the beam, but with second-order aberrations being removed from the reference component prior to recombination of the information and reference components. The wavefront of the reference component that recombines with the information component is a substantially unaberrated version of the wavefront of the beam whose wavefront is to be monitored.
    Type: Grant
    Filed: September 26, 1985
    Date of Patent: January 20, 1987
    Assignee: Lockheed Missiles & Space Company, Inc.
    Inventors: Michael E. Stefanov, Brian J. Sullivan, Anthony J. Ticknor
  • Patent number: 4624569
    Abstract: A real-time diffraction interferometer for analyzing an optical beam comprises converging means (13) for bringing the beam to a focus at focal point (14), and an apertured grating structure (20) positionable adjacent the focal point (14). The apertured grating structure (20) comprises a transparent substrate (10'), an obverse surface of which is coated with a translucent coating (11) except for a pinhole-sized spot (12) that is left uncoated so as to function as an aperture in the coating (11). A reverse surface of the substrate (10') has a lenticulate surface configuration, which functions as a diffraction grating. The beam incident upon the apertured grating structure (20) is separated into a major portion, which is transmitted with attenuated intensity through the translucent coating (11), and a minor portion, which is transmitted with undiminished intensity through the pinhole aperture (12).
    Type: Grant
    Filed: July 18, 1983
    Date of Patent: November 25, 1986
    Assignee: Lockheed Missiles & Space Company, Inc.
    Inventor: Osuk Y. Kwon
  • Patent number: 4621924
    Abstract: An apparatus for indicating misalignment of the optical elements of an optical system (10) comprises a source (11 ) of optical radiation (which is in general nonpolarized), a beam splitter (12), an optical flat (13) and an off-axis beam sampling device (14). The beam splitter (12) divides an input beam (20) from the source (11) into a transmitted component (21) which passes along the optic axis of the optical system (10) to the optical flat (13), and a reflected component (22) which passes to the off-axis beam sampling device (14). The beam sampling device (14) divides the reflected component (22) of the input beam (20) into two angularly separated beams (24) and (25), which are returned to the beam splitter (12). The beam splitter (12) transmits components (24') and (25'), respectively, of the angularly separated beams (24) and (25) to a detector plane (23).
    Type: Grant
    Filed: December 17, 1984
    Date of Patent: November 11, 1986
    Assignee: Lockheed Missiles & Space Company, Inc.
    Inventor: Samuel G. L. Williams
  • Patent number: 4621256
    Abstract: A shaft angle encoder comprises a code disc (21) mountable coaxially upon a rotary shaft (20) whose angular position is to be continuously measured. Coarse-bit angular position data are encoded digitally in Gray code by a pattern of opaque and transparent sectors provided on a plurality of inner annular tracks on the code disc (21). Fine-bit angular position data are encoded in analog triangular waveforms generated by the outermost annular track on the code disc (21). The analog position data are converted to fine-bit digital values, which are combined with coarse-bit digital values to obtain an angular position measurement. Alignment of the fine-bit digital values with the coarse-bit digital values obtained from the Gray code position data is accomplished by using information provided by overlapping the least significant bit of the coarse-bit digital values with the most significant bit of the fine-code digital values.
    Type: Grant
    Filed: September 13, 1985
    Date of Patent: November 4, 1986
    Assignee: Lockheed Missiles & Space Company, Inc.
    Inventor: Stanley J. Rusk
  • Patent number: 4609822
    Abstract: A rugged Fabry-Perot interferometer comprises a solid etalon (15) made of single-crystal silicon with precisely parallel stacks (13) and (14) of dielectric materials coated on opposite sides thereof. The stacks (13) and (14) are identical to each other, and each stack comprises a plurality of layers of different materials having alternately high and low indices of refraction. A dielectric ring (30) made of the same material as the etalon (15) is bonded to a peripheral portion of one side of the etalon (15) by an epoxy material having the same coefficient of thermal expansion as the ring (30) and the etalon (15). The ring (30) with the etalon (15) bonded thereto is kinematically mounted on Teflon contact members (34) within an annular receiving structure (31) made of a metal (such as copper) of high thermal conductivity.
    Type: Grant
    Filed: November 5, 1984
    Date of Patent: September 2, 1986
    Assignee: Lockheed Missiles & Space Company, Inc.
    Inventor: Aiden E. Roche
  • Patent number: 4605347
    Abstract: A drill/reamer bit is described that is particularly suitable for high speed operation and which comprises a bit having a "split" pilot or drill portion with four facets and two cutting edges on each web and a "step" or reamer portion having two reliefs and one cutting edge associated with each web, the webs being formed by a pair of flutes angled at from approximately 81/2.degree. to approximately 23.degree., the bit being formed primarily of fine grain tungsten carbide material, the drill portion having an included angle of approximately 118.+-.2 degrees.
    Type: Grant
    Filed: December 27, 1982
    Date of Patent: August 12, 1986
    Assignees: Lockheed Missiles & Space Company, Inc., National Carbide Tool, Inc.
    Inventors: Marvin S. Jodock, Fred Maternus
  • Patent number: 4596609
    Abstract: A thermomechanical method for forging a precipitation-hardenable aluminum alloy workpiece comprises the steps of: (1) solution heat treating the workpiece to achieve a substantially homnogeneous supersaturated solid solution of the alloy throughout the workpiece; (2) partially aging the workpiece at a temperature sufficient to cause second-phase precipitate particles to form in the workpiece, the aging of the workpiece continuing until the precipitate particles acquire a size sufficient to restrict dislocation movement in the workpiece during subsequent forging without substantially hindering workability of the alloy; and (3) mechanically working the workpiece isothermally at the temperature at which aging of the workpiece occurred.
    Type: Grant
    Filed: March 14, 1984
    Date of Patent: June 24, 1986
    Assignee: Lockheed Missiles & Space Company, Inc.
    Inventor: Elliott H. Rennhack
  • Patent number: 4595262
    Abstract: A set of safety goggles (20) for adjustably attenuating the intensity of optical radiation at any selected wavelength produced by a variable-wavelength laser (e.g., a dye laser) comprises a pair of oculars, both of which can be tuned to any particular wavelength producible by the laser. Each ocular comprises a birefringent filter, which includes stationary components including a polarizer (11), a wide-field element made up of a half-wave plate (13) sandwiched between multiwave plates (12 and 14), and a quarter-wave plate (16), and rotatable components including a polarizer (18). The wide-field element causes an optical path difference between orthogonal components of a single polarization state. The quarter-wave plate (15) and the rotatable polarizer (18) in combination enable selection of any particular wavelength whose intensity is to be attenuated.
    Type: Grant
    Filed: August 23, 1984
    Date of Patent: June 17, 1986
    Assignee: Lockheed Missiles & Space Company, Inc.
    Inventor: Norman E. Ogle, deceased
  • Patent number: 4585996
    Abstract: An instrument for measuring electrical conductivity of a liquid comprises a two-electrode probe for insertion into the liquid. A triangular waveform generator (IC4 and IC5) impresses a voltage of fixed amplitude on one electrode of the probe by means of driver circuitry (IC3). This voltage drives an electric current through the liquid to the other electrode of the probe. Receiver circuitry (IC6) detects the current at this other electrode, and converts the detected current to a triangular wavefore AC voltage signal. Amplifier circuitry (IC1) amplifies the output of the receiver circuitry, and the amplified voltage signal is converted to a smoothed DC voltage signal by precision rectifier circuitry (IC2 and IC7). The output of the precision rectifier circuitry is processed to obtain a signal indicative of electrical conductivity of the liquid.
    Type: Grant
    Filed: May 27, 1983
    Date of Patent: April 29, 1986
    Assignee: Lockheed Missiles & Space Company, Inc.
    Inventor: Robert S. Luce
  • Patent number: 4583855
    Abstract: An apparatus is described for measuring spatial phase difference between a signal beam and a reference beam in substantially real time, where the signal and reference beams are coherent beams of optical radiation superimposed upon each other and having orthogonal polarization states with respect to each other.
    Type: Grant
    Filed: February 17, 1984
    Date of Patent: April 22, 1986
    Assignee: Lockheed Missiles & Space Company, Inc.
    Inventor: Noah Bareket